CN108759793A - A kind of mapping unmanned plane convenient for angular adjustment - Google Patents

A kind of mapping unmanned plane convenient for angular adjustment Download PDF

Info

Publication number
CN108759793A
CN108759793A CN201810203260.7A CN201810203260A CN108759793A CN 108759793 A CN108759793 A CN 108759793A CN 201810203260 A CN201810203260 A CN 201810203260A CN 108759793 A CN108759793 A CN 108759793A
Authority
CN
China
Prior art keywords
gear
mapping
measuring arm
unmanned plane
gondola
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201810203260.7A
Other languages
Chinese (zh)
Inventor
黄少琼
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Qingyuan Jujin Technology Co Ltd
Original Assignee
Qingyuan Jujin Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Qingyuan Jujin Technology Co Ltd filed Critical Qingyuan Jujin Technology Co Ltd
Priority to CN201810203260.7A priority Critical patent/CN108759793A/en
Publication of CN108759793A publication Critical patent/CN108759793A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C15/00Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Transmission Devices (AREA)

Abstract

The present invention has opened a kind of mapping unmanned plane convenient for angular adjustment,Including drone body,The inside for measuring gondola is equipped with electric hydaulic bar,The top of the electric hydaulic bar is equipped with servo motor,The top of the servo motor is equipped with first gear,Rack is installed on the inside of the fixed protective shell top,The first gear engages connection with rack,It is provided with connector sleeve at the top of the fixed protective shell,The side of the connector sleeve offers arc groove,The inside is equipped with probe rod,The top of the probe rod is equipped with second gear,The external engagement of the second gear is connected with gear band,The top of the connector sleeve is separately installed with left measuring arm and right measuring arm,Sliding rail is installed on the measurement gondola wall of the left measuring arm and right measuring arm bottom,The angle of mapping probe can be adjusted flexibly in the present invention,To improve the mapping precision of mapping unmanned plane,Operation is simple and reliable.

Description

A kind of mapping unmanned plane convenient for angular adjustment
Technical field
The present invention relates to unmanned plane, specially a kind of mapping unmanned planes convenient for angular adjustment.
Background technology
Commonly the mode of surveying and drawing includes that the mapping on the spot of staff, unmanned plane mapping and satellite are distant in Modern Surveying & Mapping work Sensing such as paints at the modes, but less efficient by way of staff's field survey, and needs to expend a large amount of human resources, And then there is measurement accuracy in satellite remote sensing, therefore unmanned plane mapping is played in Modern Surveying & Mapping work and is increasingly weighed The effect wanted;Mapping unmanned plane in the prior art usually installs left mapping probe and right mapping probe in the bottom surface of unmanned plane, But the position of probe is relatively fixed, and cannot flexibly be adjusted as needed, therefore can only just have been thought by manipulating unmanned plane change Come achieve the purpose that improve measurement accuracy, operation it is relatively complicated, be unfavorable for using.
So how to design a kind of mapping unmanned plane convenient for angular adjustment, becoming us will currently solve the problems, such as.
Invention content
The purpose of the present invention is to provide a kind of mapping unmanned planes convenient for angular adjustment, to solve in above-mentioned background technology The problem of proposition.
To achieve the above object, the present invention provides the following technical solutions:A kind of mapping unmanned plane convenient for angular adjustment, packet Include drone body, empennage, start pulley, measure gondola, electric hydaulic bar, servo motor, first gear, fixed protective shell, Rack, connector sleeve, arc groove, probe rod, rolling bearing, second gear, postive stop baffle, limited block, mapping probe, left measurement Arm, right measuring arm, sliding rail and gear band are equipped with empennage, the drone body bottom at the top of described drone body one end The both ends in portion are equipped with startup pulley, and measurement gondola is equipped in the middle part of the drone body bottom end, the measurement gondola Inside is equipped with electric hydaulic bar, and the top of the electric hydaulic bar is equipped with servo motor, the top peace of the servo motor Equipped with first gear, the both sides of the first gear are mounted on fixed protective shell, the inside peace on the fixed protective shell top Equipped with rack, the first gear engages connection with rack, and connector sleeve, the connection are provided at the top of the fixed protective shell The side of set offers arc groove, and the inside is equipped with probe rod, and the bottom of the probe rod is equipped with rolling bearing, institute The top for stating probe rod is equipped with second gear, and the external engagement of the second gear is connected with gear band, the fixed protection The side of shell is equipped with postive stop baffle, and limited block is equipped on the measurement gondola, and the bottom end of the probe rod is equipped with survey Probe is painted, the top of the connector sleeve is separately installed with left measuring arm and right measuring arm, the left measuring arm and right measuring arm bottom Sliding rail is installed on the measurement gondola wall in portion.
Further, the other end of the gear band is connect by fixed gear with left measuring arm.
Further, the half of the gear strip length is more than the distance between left measuring arm upper limit baffle.
Further, the gear band is inside and outside with gear band with teeth.
Further, the outside of the mapping probe is provided with transparent protective shield.
Further, the measurement gondola is a kind of component of stainless steel.
Compared with prior art, the beneficial effects of the invention are as follows:In use, when needing laterally moved, lead to The work of external control switch control servomotor is crossed, first gear rotation, first gear band carry-over bar is driven to move, so that The movement of left measuring arm and right measuring arm achievees the purpose that make mapping probe transverse shifting, when needing to carry out angle to mapping probe When degree adjustment, electric hydaulic bar is controlled by external switch and is shunk, first gear drops to arc groove, starts motor, drives the Two gears rotate, and second gear drives mapping probe rotation, and to achieve the purpose that adjust mapping probe angle, the present invention can spirit The angle of adjustment mapping probe living, to improve the mapping precision of mapping unmanned plane, operation is simple and reliable.
Description of the drawings
Attached drawing is used to provide further understanding of the present invention, and a part for constitution instruction, the reality with the present invention It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings:
Fig. 1 is overall structure of the present invention;
Fig. 2 is mounting structure of servo motor schematic diagram of the present invention;
Fig. 3 is connecting jacket structure schematic diagram of the present invention;
Fig. 4 is that the present invention measures gondola vertical view;
Figure label:1, drone body;2, empennage;3, start pulley;4, gondola is measured;5, electric hydaulic bar;6, it watches Take motor;7, first gear;8, fixed protective shell;9, rack;10, connector sleeve;11, arc groove;12, probe rod;13, the axis of rolling It holds;14, second gear;15, postive stop baffle;16, limited block;17, mapping probe;18, left measuring arm;19, right measuring arm; 20, sliding rail;21, gear band.
Specific implementation mode
Hereinafter, preferred embodiments of the present invention will be described with reference to the accompanying drawings, it should be understood that preferred reality described herein Apply example only for the purpose of illustrating and explaining the present invention and is not intended to limit the present invention.
- 4 are please referred to Fig.1, the present invention provides a kind of technical solution:A kind of mapping unmanned plane convenient for angular adjustment, including Drone body 1, empennage 2 start pulley 3, measure gondola 4, electric hydaulic bar 5, servo motor 6, first gear 7, fixed guarantor Protective case 8, rack 9, connector sleeve 10, arc groove 11, probe rod 12, rolling bearing 13, second gear 14, postive stop baffle 15, limit Block 16, mapping probe 17, left measuring arm 18, right measuring arm 19, sliding rail 20 and gear band 21, the top of 1 one end of drone body Portion is equipped with empennage 2, and the both ends of 1 bottom of drone body, which are equipped with, starts pulley 3, the middle part installation of 1 bottom end of drone body Have and measure gondola 4, the inside for measuring gondola 4 is equipped with electric hydaulic bar 5, and the top of electric hydaulic bar 5 is equipped with servo motor 6, the top of servo motor 6 is equipped with first gear 7, and the both sides of first gear 7 are mounted on fixed protective shell 8, fixed protection Rack 9 is installed, first gear 7 engages connection with rack 9, and the top of fixed protective shell 8 is provided with connection on the inside of 8 top of shell Set 10, the side of connector sleeve 10 offers arc groove 11, inside probe rod 12 is installed, the bottom of probe rod 12 is equipped with rolling The top of dynamic bearing 13, probe rod 12 is equipped with second gear 14, and the external engagement of second gear 14 is connected with gear band 21, Gu The side for determining protective shell 8 is equipped with postive stop baffle 15, measures and is equipped with limited block 16 on gondola 4, the bottom end peace of probe rod 12 Equipped with mapping probe 17, the top of connector sleeve 10 is separately installed with left measuring arm 18 and right measuring arm 19, left measuring arm 18 and the right side Sliding rail 20 is installed on 4 wall of measurement gondola of 19 bottom of measuring arm.
Further, the other end of gear band 21 is connect by fixed gear with left measuring arm 18, and being convenient for transmission makes With.
Further, the half of 21 length of gear band is more than the distance between 18 upper limit baffle 15 of left measuring arm, ensures The performance of gear band 21.
Further, gear band 21 is inside and outside with gear band with teeth, ensure inside and outside can be all driven.
Further, the outside of mapping probe 17 is provided with transparent protective shield, can preferably be protected to mapping probe 17 Shield, improves its service life.
Further, it is a kind of component of stainless steel to measure gondola 4, ensures to measure the physical property of gondola 4 and resistance to Corrosive nature.
Operation principle:In use, when needing laterally moved, pass through external control switch control servomotor 6 work, drive first gear 7 to rotate, and first gear 7 is moved with carry-over bar 9, so that left measuring arm 18 and right measuring arm 19 Movement, achieve the purpose that make 17 transverse shifting of mapping probe, when need to mapping probe 17 carry out angle adjustment when, by outer Portion's switch control electric hydaulic bar 5 is shunk, and first gear 7 drops to arc groove 11, starts motor, drives 14 turns of second gear Dynamic, second gear 14 drives mapping probe 17 to rotate, and to achieve the purpose that adjust 17 angle of mapping probe, the present invention can be flexible The angle for adjusting mapping probe 17, to improve the mapping precision of mapping unmanned plane, operation is simple and reliable.
Finally it should be noted that:The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used With technical scheme described in the above embodiments is modified or equivalent replacement of some of the technical features. All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in the present invention's Within protection domain.

Claims (6)

1. a kind of mapping unmanned plane convenient for angular adjustment, including drone body (1), empennage (2), startup pulley (3), measurement Gondola (4), electric hydaulic bar (5), servo motor (6), first gear (7), fixed protective shell (8), rack (9), connector sleeve (10), arc groove (11), probe rod (12), rolling bearing (13), second gear (14), postive stop baffle (15), limited block (16), mapping probe (17), left measuring arm (18), right measuring arm (19), sliding rail (20) and gear band (21), it is characterised in that: Empennage (2) is installed, the both ends of drone body (1) bottom, which are equipped with, opens at the top of described drone body (1) one end Movable pulley (3) is equipped in the middle part of drone body (1) bottom end and measures gondola (4), the inside for measuring gondola (4) Electric hydaulic bar (5) is installed, the top of the electric hydaulic bar (5) is equipped with servo motor (6), the servo motor (6) Top first gear (7) is installed, the both sides of the first gear (7) are mounted on fixed protective shell (8), described fixed to protect Rack (9) is installed, the first gear (7) engages connection, the fixed protection with rack (9) on the inside of protective case (8) top Connector sleeve (10) is provided at the top of shell (8), the side of the connector sleeve (10) offers arc groove (11), inside peace Equipped with probe rod (12), the bottom of the probe rod (12) is equipped with rolling bearing (13), the top peace of the probe rod (12) Equipped with second gear (14), the external engagement of the second gear (14) is connected with gear band (21), the fixed protective shell (8) Side postive stop baffle (15) is installed, limited block (16) is installed on the measurement gondola (4), the probe rod (12) Bottom end is equipped with mapping probe (17), and the top of the connector sleeve (10) is separately installed with left measuring arm (18) and right measuring arm (19), sliding rail (20) is installed on measurement gondola (4) wall of the left measuring arm (18) and right measuring arm (19) bottom.
2. a kind of mapping unmanned plane convenient for angular adjustment according to claim 1, it is characterised in that:The gear band (21) the other end is connect by fixed gear with left measuring arm (18).
3. a kind of mapping unmanned plane convenient for angular adjustment according to claim 1, it is characterised in that:The gear band (21) half of length is more than the distance between left measuring arm (18) upper limit baffle (15).
4. a kind of mapping unmanned plane convenient for angular adjustment according to claim 1, it is characterised in that:The gear band (21) it is inside and outside with gear band with teeth.
5. a kind of mapping unmanned plane convenient for angular adjustment according to claim 1, it is characterised in that:The mapping probe (17) outside is provided with transparent protective shield.
6. a kind of mapping unmanned plane convenient for angular adjustment according to claim 1, it is characterised in that:The measurement gondola (4) it is a kind of component of stainless steel.
CN201810203260.7A 2018-03-13 2018-03-13 A kind of mapping unmanned plane convenient for angular adjustment Pending CN108759793A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810203260.7A CN108759793A (en) 2018-03-13 2018-03-13 A kind of mapping unmanned plane convenient for angular adjustment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810203260.7A CN108759793A (en) 2018-03-13 2018-03-13 A kind of mapping unmanned plane convenient for angular adjustment

Publications (1)

Publication Number Publication Date
CN108759793A true CN108759793A (en) 2018-11-06

Family

ID=63980309

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810203260.7A Pending CN108759793A (en) 2018-03-13 2018-03-13 A kind of mapping unmanned plane convenient for angular adjustment

Country Status (1)

Country Link
CN (1) CN108759793A (en)

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3210946A1 (en) * 1982-03-25 1983-10-06 Dirk Fuehrmann Rotating-wing aircraft
KR20020015404A (en) * 2000-08-22 2002-02-28 사태형 Propelling equipment and balloon of airship
CN206155793U (en) * 2016-11-09 2017-05-10 于华 Survey and drawing unmanned aerial vehicle
CN206280683U (en) * 2016-12-01 2017-06-27 中国科学院地理科学与资源研究所 Unmanned plane rotary head multi-angle oblique camera
CN107196034A (en) * 2017-06-05 2017-09-22 东莞质研工业设计服务有限公司 A kind of unmanned plane
CN107253529A (en) * 2017-06-23 2017-10-17 深圳市雷凌广通技术研发有限公司 A kind of unmanned plane for sea garbage-cleaning based on Internet of Things
CN206797760U (en) * 2017-05-17 2017-12-26 天津经天航空科技有限公司 A kind of new unmanned plane device
CN207015575U (en) * 2017-06-05 2018-02-16 河北天海测绘服务有限公司 Take photo by plane unmanned plane
CN207045735U (en) * 2017-08-01 2018-02-27 四川省冶地工程勘察设计有限公司 One kind mapping unmanned plane
CN207060417U (en) * 2017-07-07 2018-03-02 张丽娟 A kind of unmanned plane cradle head device of replaceable camera
CN107745801A (en) * 2017-10-18 2018-03-02 柳良红 One kind, which is taken photo by plane, surveys and draws unmanned plane

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3210946A1 (en) * 1982-03-25 1983-10-06 Dirk Fuehrmann Rotating-wing aircraft
KR20020015404A (en) * 2000-08-22 2002-02-28 사태형 Propelling equipment and balloon of airship
CN206155793U (en) * 2016-11-09 2017-05-10 于华 Survey and drawing unmanned aerial vehicle
CN206280683U (en) * 2016-12-01 2017-06-27 中国科学院地理科学与资源研究所 Unmanned plane rotary head multi-angle oblique camera
CN206797760U (en) * 2017-05-17 2017-12-26 天津经天航空科技有限公司 A kind of new unmanned plane device
CN107196034A (en) * 2017-06-05 2017-09-22 东莞质研工业设计服务有限公司 A kind of unmanned plane
CN207015575U (en) * 2017-06-05 2018-02-16 河北天海测绘服务有限公司 Take photo by plane unmanned plane
CN107253529A (en) * 2017-06-23 2017-10-17 深圳市雷凌广通技术研发有限公司 A kind of unmanned plane for sea garbage-cleaning based on Internet of Things
CN207060417U (en) * 2017-07-07 2018-03-02 张丽娟 A kind of unmanned plane cradle head device of replaceable camera
CN207045735U (en) * 2017-08-01 2018-02-27 四川省冶地工程勘察设计有限公司 One kind mapping unmanned plane
CN107745801A (en) * 2017-10-18 2018-03-02 柳良红 One kind, which is taken photo by plane, surveys and draws unmanned plane

Similar Documents

Publication Publication Date Title
US10161816B2 (en) Torque sensors
US10926404B2 (en) Gear packaging for robot arms
US10792820B2 (en) Drive arrangements for robot arms
WO2007076731B1 (en) Method and apparatus for measurement and/or calibration of position of an object in space
GB2540756A (en) Gear packaging for robot arms
CN207045735U (en) One kind mapping unmanned plane
CN108204782A (en) A kind of angle measurement and instruction device based on Archimedian screw disk
CN106840584B (en) Multi-degree-of-freedom sub-span supersonic wind tunnel large attack angle mechanism
US9796461B2 (en) Pitch angle indicator system
CN114217407B (en) Adjusting structure of lens and head-mounted display device
CN106524889A (en) Pull rod linear displacement sensor
CN108759793A (en) A kind of mapping unmanned plane convenient for angular adjustment
CN107703601A (en) A kind of reflective mirror regulating mechanism
CN203738787U (en) Mechanical arm with testing heads controlled to accurately move and be positioned in XY plane
CN107830822A (en) A kind of opto-electrical angle measuring apparatus
CN203848822U (en) Series-wound electronic horizontal measuring instrument
CN207489501U (en) Collimator
CN208369386U (en) A kind of electric cylinder of inbuilt displacement sensor and precise ball screw
CN209725138U (en) A kind of inner circulation structure ball screw assembly,
CN109256233B (en) A pipe auto-change over device for neutron scattering spectrometer
WO2020103437A1 (en) Optical stop position detection apparatus and medical accelerator treatment head
CN105252937B (en) A kind of improved precision locating tab assembly compasses
CN108168534A (en) A kind of algorithm accurately MEMS gyroscope
CN205898161U (en) Attack angle sensor ware calibrating device
CN207963896U (en) A kind of algorithm accurately MEMS gyroscope

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20181106

RJ01 Rejection of invention patent application after publication